JP3736205B2 - Battery power storage device - Google Patents

Battery power storage device Download PDF

Info

Publication number
JP3736205B2
JP3736205B2 JP15779799A JP15779799A JP3736205B2 JP 3736205 B2 JP3736205 B2 JP 3736205B2 JP 15779799 A JP15779799 A JP 15779799A JP 15779799 A JP15779799 A JP 15779799A JP 3736205 B2 JP3736205 B2 JP 3736205B2
Authority
JP
Japan
Prior art keywords
storage battery
voltage
charging
cell
charging current
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
JP15779799A
Other languages
Japanese (ja)
Other versions
JP2000350378A5 (en
JP2000350378A (en
Inventor
正芳 後藤
敏夫 郷内
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Mitsubishi Electric Corp
Original Assignee
Mitsubishi Electric Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Mitsubishi Electric Corp filed Critical Mitsubishi Electric Corp
Priority to JP15779799A priority Critical patent/JP3736205B2/en
Priority to US09/443,286 priority patent/US6373224B1/en
Priority to FR9915100A priority patent/FR2794578B1/en
Priority to EP00108803A priority patent/EP1058367B1/en
Priority to CA002310357A priority patent/CA2310357C/en
Publication of JP2000350378A publication Critical patent/JP2000350378A/en
Publication of JP2000350378A5 publication Critical patent/JP2000350378A5/ja
Application granted granted Critical
Publication of JP3736205B2 publication Critical patent/JP3736205B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Images

Classifications

    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J7/00—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
    • H02J7/0013—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries acting upon several batteries simultaneously or sequentially
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J7/00—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
    • H02J7/34—Parallel operation in networks using both storage and other dc sources, e.g. providing buffering
    • H02J7/35—Parallel operation in networks using both storage and other dc sources, e.g. providing buffering with light sensitive cells
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00—Energy generation through renewable energy sources
    • Y02E10/50—Photovoltaic [PV] energy
    • Y02E10/56—Power conversion systems, e.g. maximum power point trackers
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00—Road transport of goods or passengers
    • Y02T10/60—Other road transportation technologies with climate change mitigation effect
    • Y02T10/70—Energy storage systems for electromobility, e.g. batteries

Description

【０００１】
【発明の属する技術分野】
この発明は、例えば低高度衛星用電源装置及び電気自動車用電源装置等に使用されるバッテリ蓄電装置に関するものである。
なおここでは説明の便宜上、低高度衛星用電源装置について説明する。
【０００２】
図６は、従来のNiCd（ニッケルカドミウム）バッテリ等の蓄電池を使用した低高度衛星用電源装置の構成図であり、図６において、１は太陽電池、２は太陽電池１で発生した余剰電力を消費するシャント装置、３は太陽電池１の電流をシャント装置２を介して入力し、充電制御器４ａと負荷６へ電流を供給するとともに太陽電池１の発生電力が低下した場合には、蓄電池５の放電により負荷６へ電流を供給するように充電制御器４ａを制御する電力制御器である。充電制御器４ａは、電力制御器３の出力を受けて、蓄電池５へ電流を供給して充電させ、また太陽電池１の発生電力が低下した場合の信号で蓄電池５を放電させるための充電制御器である。７は逆流防止ダイオードである。
【０００３】
従来の低高度衛星用電源装置の動作を以下に説明する。
太陽電池１からの電流は逆流防止ダイオード７、シャント装置２を介して電力制御器３に入力される。電力制御器３は日照時において得られる太陽電池１からの電流を負荷６と充電制御器４ａに供給する。充電制御器４ａでは電力制御器３からの電力により図７（ｃ）に示す一定の電流Ｉ0を生成し、この電流Ｉ0を蓄電池５に供給して、蓄電池５を充電する。蓄電池５の電圧は充電の進行に伴い図７（ｂ）に示すように上昇する。蓄電池５の電圧が図７（ａ）に示すように予め設定してある温度補償された電圧値（これをＶ−Ｔカーブと呼び、要求により１本からｎ本設定する）に達したことを充電制御器４ａで検出すると充電制御器４はそれまでの定電流充電から定電圧充電へ移行する。これにより充電電流は図７（ｃ）に示すようにテーパ状に減少し、蓄電池５への過充電を防止する。
一方、日陰時において太陽電池１の発生電力が低下した場合、上記充電制御器４ａは電力制御器３の出力により蓄電池５を放電し、負荷６へ電力を供給する。
【０００４】
【発明が解決しょうとする課題】
従来の低高度衛星用電源装置における蓄電池の充電は、上記のように行われているが、上記のような定電圧／定電流充電はｎ個の蓄電池セルを直列に縦続接続した蓄電池全体に対して行われるため、蓄電池を構成する各セルの充電特性のアンバランスにより蓄電池内の特定のセルが過充電されるという問題点があった。特にLi（リチウム）系電極で構成されるLi-Ion（リチウム・イオン）セルは、エネルギー密度、充電電圧、放電電圧等がNiCdセルに比べて高く、蓄電池への使用が期待されているが、 Li-Ionセルの場合、規定電圧を越えて過充電状態になると電極劣化が促進され、寿命が短くなってしまう問題点がある。例えば、温度Ｔｏ°Ｃの時のＶ−Ｔカーブにおける定電圧動作電圧は、ｎ個のセル電圧の和を蓄電池電圧として検出し、設定電圧と比較動作するが、ｍ個目のセル電圧が他のセル電圧よりもセルの内部抵抗の関係で高くなっている場合、セルの上限電圧を超えてしまい、その結果当該セルを劣化させてしまうことがあった。
【０００５】
この発明は、かかる課題を解決するためになされたものであり、蓄電池を構成する個々のセルが過充電とならず適切な充電量が確保できるバッテリ蓄電装置を得ることを目的とするものである。
【０００６】
【課題を解決するための手段】
第１の発明によるバッテリ蓄電装置は、蓄電池セルが縦続接続された蓄電池と、電源出力から上記蓄電池を充電するための異なる複数の充電電流を生成し、異なる規定電圧値になるまで上記蓄電池に異なる複数の充電電流を供給する手段を有する充電電流生成手段とを備えたものである。
【０００７】
第２の発明によるバッテリ蓄電装置は、第１の発明において充電電流生成手段に、異なる複数の充電電流を生成し、かつ上記充電電流は、最初高いレベルで供給した後、低いレベルで供給するように充電電流を変化させる手段を設けたものである。
【０００８】
第３の発明によるバッテリ蓄電装置は、第１、第２の発明において充電電流生成手段に、各蓄電池セルの電圧のいずれかが規定の電圧に達したとき充電電流を高いレベルから低いレベルに変化させる手段を設けたものである。
【０００９】
第４の発明によるバッテリ蓄電装置は、第１〜第３の発明において 各蓄電池セルにそれぞれシャント回路を接続し、蓄電池への最低レベルの充電電流供給状態でいずれかの蓄電池セルの電圧が規定の電圧に達した場合、当該蓄電池セルに流れる充電電流を当該蓄電池セルに接続されたシャント回路へバイパスするようにしたものである。
【００１０】
第５の発明によるバッテリ蓄電装置は、第１〜第４の発明において 電源と蓄電池との間に設けられ、通常はＯＮし、かつ上記蓄電池セルの電圧のいずれかが規定電圧に達したとき、上記充電電流生成手段によりＯＦＦされ、放電によりＯＮに復帰するスイッチを設けたものである。
【００１１】
第６の発明によるバッテリ蓄電装置は、第１〜第５の発明において上記充電電流生成手段に、上記蓄電池セル全体の電圧を検出し、その検出した電圧が規定電圧に達したときに定電圧充電制御に移行する手段を設けたものである。
【００１２】
第７の発明によるバッテリ蓄電装置は、第１〜第６の発明において上記充電電流生成手段に、上記複数の蓄電池セル電圧がアンバランスになったとき定電圧充電制御を解除し、低レベルの充電電流で規定電圧に達するまで充電する手段を設けたものである。
【００１３】
第８の発明によるバッテリ蓄電装置は、第１〜第７の発明において上記蓄電池セルとしてLi（リチウム）系電極で構成されるLi-Ion（リチウムイオン）蓄電池セルを用いたものである。
【００１４】
【発明の実施の形態】
実施の形態１．
図１は、この発明の実施の形態１を示す低高度衛星用電源装置の構成図である。図１において、１、２、３、５、６、７は図６と同様である。４ｂは充電用太陽電池９の出力に基づき複数の充電電流を生成し、蓄電池セルが縦続接続された蓄電池５へ異なる複数の充電電流を供給する充電制御器、８は充電用太陽電池９と蓄電池５との間に接続され逆流防止ダイオード、１０は蓄電池５と逆流防止ダイオード８との間に接続されたスイッチで、充電開始時はＯＮの状態であり、充電用太陽電池９から直接蓄電池５へ充電が行われる。１１は制御用ダイオードである。
なお、充電制御器４ｂは、充電用太陽電池９の出力に基づく充電電流Ｉ１よりレベルの低い充電電流Ｉ２、Ｉ３（Ｉ２＞Ｉ３）を生成する電流制御部を有している。
１２は各蓄電池セルにそれぞれ対応して設けられ、各蓄電池セルの電圧を検出し、かつ当該検出した蓄電池セルの電圧が規定電圧に達した場合、所定の信号を出力する複数のセル電圧検出器、１３は上記複数のセル電圧検出器１２の出力端に接続され、セル電圧検出器１２からの所定信号を上記充電制御器４ｂへ出力するＯＲ回路である。
【００１５】
次にこの発明の動作を以下に説明する。
充電用太陽電池９からの充電電流Ｉ１（例えば３０Ａ）が図２（ａ）のＩ１に示すようにスイッチ１０を介して蓄電池５に供給されると、蓄電池５の各蓄電池セルが充電されて各蓄電池セルの電圧が図２（ｂ）のアに示すように上昇する。セル電圧検出器１２は蓄電池セルの電圧をそれぞれ検出するが、複数の蓄電池セルのいずれかのセル電圧が規定電圧（例えば３．９８Ｖ）に達したとき当該セル電圧を検出しているセル電圧検出器１２から例えばＨｉｇｈレベルの信号をＯＲ回路１３へ出力する。充電制御器４ｂは上記セル電圧検出器１２から出力されたＨｉｇｈレベルの信号をＯＲ回路１３を介して入力したときＯＮ状態のスイッチ１０をＯＦＦに切替える信号を制御用ダイオード１１を介してスイッチ１０へ出力し、スイッチ１０をＯＦＦとする。また充電制御器４ｂは、全体の蓄電池セル電圧が規定電圧（例えば３．９５Ｖ×蓄電池セル数）に達したときスイッチ１０をＯＦＦにして定電圧充電に移行させるようになっている。
さらに充電制御器４ｂは、上記充電用太陽電池９からの出力に基づき充電電流Ｉ１より低いレベルの充電電流Ｉ２、Ｉ３（ Ｉ２＞Ｉ３）を生成する機能（充電電流Ｉ１を充電電流Ｉ２、Ｉ３に切替える機能）を有し、スイッチ１０のＯＦＦと同時に例えば５Ａの充電電流Ｉ２（図２（ａ）のＩ２参照）を蓄電池５に供給し、各蓄電池セルを充電する。この時、各蓄電池セルの充電電圧は、図２（ｂ）のイに示すように初めは減少するが、やがて上昇する。Ｉ２の充電電流により各蓄電池セルが充電され、複数の蓄電池セルのうちいずれかのセル電圧が規定電圧（例えば３．９８Ｖ）に達した場合、これをセル電圧検出器１２により検出され、その信号がＯＲ回路１３を介して充電制御器４ｂに入力される。充電制御器４ｂはセル電圧検出器１２からの信号を受けて上記Ｉ２をＩ３の充電電流に切替えて蓄電池５へ図２（ａ）に示すＩ３の充電電流（例えば１Ａ）を供給し、各蓄電池セルを充電する（図２（ｂ）のウ参照）。
なお、充電制御器４ｂは、蓄電池５の放電時にスイッチ１０をＯＮに復帰させる信号を制御用ダイオード１１を介してスイッチ１０へ出力するようになっている。
【００１６】
以上のように この発明は、蓄電池に異なる複数の充電電流を供給し、当該充電電流は、最初高いレベルで供給した後、次に低いレベルで供給するようにした多段充電機能を設けたので、充電制御器は充電用太陽電池の電力より低いレベルの充電電流を制御すればよく充電効率が向上するとともに、小型、軽量化できるという効果がある。
また、さらに低レベルの充電電流を設定することにより木目細かく充電制御できる。
【００１７】
実施の形態２．
図３はこの発明の実施の形態２を示す低高度衛星用電源装置の構成図である。この実施の形態２は、上記実施の形態２の構成のものにシャント回路１４を各蓄電池セルに並列に接続し、蓄電池セルの電圧が規定電圧に達した場合、充電電流を規定電圧に達した蓄電池セルに並列接続したシャント回路１４にバイパスさせて当該蓄電池セルの電圧上昇を抑えるように構成したところに特徴を有する。
充電電流Ｉ３により充電されている場合においてセル電圧検出器１２は蓄電池セルの電圧が規定電圧に達していない場合Ｌｏｗレベルの信号を出力する。シャント回路１４はこのＬｏｗレベルの信号が出力されている場合はＯＦＦ状態となっていて蓄電池セルに充電電流Ｉ３が流れる。一方セル電圧検出器１２は蓄電池セルの電圧が規定電圧に達した場合Ｈｉｇｈレベルの信号を出力する。シャント回路１４はこのＨｉｇｈレベルの信号によりＯＮとなる。これにより充電電流は規定電圧に達した蓄電池セルに並列接続されたシャント回路１４にバイパスされて消費するため、当該蓄電池セルに充電電流Ｉ３が流れなくなり電圧上昇を抑制することができる。
【００１８】
以上のように この発明は、各蓄電池セル毎に上限電圧制御ができるので、蓄電池セルのサイクル寿命劣化を最小に抑えることができる。
【００１９】
実施の形態３．
図４はこの発明の実施の形態３を示す低高度衛星用電源装置の構成図である。この実施の形態３では、基本的には実施の形態２と同じであるが、実施の形態２と異なるところはＯＲ回路１９の出力に基づきスイッチ１０をオフする信号を出力する信号ダイオード１９と、充電電流Ｉ３により充電されている場合において蓄電池全体の電圧をモニターし、当該電圧が規定電圧（充電電流を切替えるための規定電圧より低く設定する）に達した場合は、定電流充電から定電圧充電に移行（切替え）させる機能を有する充電制御器４ｃを設けたものである。
なお定電圧充電は各蓄電池セル電圧がバランスしているときに生じ、バッテリ動作として理想的な状態である。
【００２０】
以上のように この発明は、充電電流Ｉ１により充電されている場合の蓄電池全体の電圧をモニターし、当該電圧が規定の電圧（例えば３．９５Ｖ×蓄電池数）に達したとき、定電流充電から定電圧充電へ切替える機能を充電制御器に持たせ、この機能を多段充電と併用することにより蓄電池セルの電圧特性がバランスしているときにできるだけシャント回路を動作させないで充電制御するようにしたので
規定電圧を低く抑えることができ、蓄電池セルのサイクル寿命劣化を低く抑えることができる。。
【００２１】
実施の形態４．
図５はこの発明の実施の形態４を示す低高度衛星用電源装置の構成図である。この実施の形態４では、基本的には実施の形態３と同じであるが、実施の形態３と異なるところは定電流充電から定電圧充電に移行した後、各蓄電池セル電圧にアンバランスが生じた場合、定電圧充電制御を解除し、各蓄電池セル電圧を強制的にシャント回路１２が動作するまで（シャント電圧まで）充電電流Ｉ３で充電させて各蓄電池セル電圧のバランスをとる機能を有する充電制御器４ｄを設けたものである。
なお上記各蓄電池セルの電圧はセル電圧検出器１２により検出され、ＯＲ回路１３を介して充電制御器４ｄに入力され、充電制御器４ｄにおいて各蓄電池セル電圧にアンバランス（規定電圧に対する各蓄電池セル相互間の電圧のばらつき）の有無を検出するようになっているが、各蓄電池セルの電圧を地上局側でモニターし、上記アンバランスが生じた場合に上記充電制御器４ｄに対し定電圧充電制御を解除し、各蓄電池セル電圧を強制的にシャント回路１２が動作するまで充電電流Ｉ３で充電させるためのコマンドを発生するようにしても良い。
【００２２】
以上のように、この発明は、定電流充電から定電圧充電に移行した後、各蓄電池セル電圧にアンバランスが生じた場合、定電圧充電制御を解除し、各蓄電池セルを充電電流Ｉ３によりシャント動作電圧まで充電することにより、充電のサイクルの進行に伴って生じる各蓄電池セル電圧のアンバランスを是正することができる。
【００２３】
なお上記各実施の形態は、低高度衛星用電源装置を例に上げて説明したが、この発明は、他の衛星、電気自動車、地上用太陽発電などにも適用できるものである。
【００２４】
【発明の効果】
この発明によれば、異なる充電電流により縦続接続された複数の蓄電池セルを充電（多段充電）することにより蓄電池セルの過充電を抑制することができる。
【００２５】
またこの発明は、蓄電池への最低レベルの充電電流供給状態でいずれかの蓄電池セルの電圧が規定の電圧に達した場合、当該蓄電池セルに流れる充電電流を当該蓄電池セルに接続されたシャント回路へバイパスするようにしたので、蓄電池セルの過充電を抑制することができる。
【００２６】
この発明は、各蓄電池セルの電圧がバランスしている状態における蓄電池全体の電圧をモニターし、当該電圧が規定電圧に達した場合は、定電流充電から定電圧充電に切替えるようにしたので、サイクル寿命劣化を抑える上でバッテリ動作を理想的な状態にすることができる。
【００２７】
またこの発明は、定電流充電から定電圧充電に移行した後、各蓄電池セル電圧にアンバランスが生じた場合、定電圧充電制御を解除し、各蓄電池セルをシャント動作電圧まで充電することにより、各蓄電池セル電圧のアンバランスを是正することができる。
【図面の簡単な説明】
【図１】 この発明の実施の形態１を示す低高度衛星用電源装置の構成図である。
【図２】 この発明の実施の形態１を示す低高度衛星用電源装置の電流、電圧特性を説明するための図である。
【図３】 この発明の実施の形態２を示す低高度衛星用電源装置の構成図である。
【図４】 この発明の実施の形態３を示す低高度衛星用電源装置の構成図である。
【図５】 この発明の実施の形態４を示す低高度衛星用電源装置の構成図である。
【図６】 従来の低高度衛星用電源装置の構成図である。
【図７】 従来の低高度衛星用電源装置の電流、電圧特性を説明するための図である。
【符号の説明】
４ 充電制御器 ５ 蓄電池 ９ 充電用太陽電池 １０ スイッチ １１ 制御用ダイオード １２ セル電圧検出器 １３ ＯＲ回路 １４シャント回路 １６ 信号用ダイオード。[0001]
BACKGROUND OF THE INVENTION
The present invention relates to a battery power storage device used in, for example, a low-altitude satellite power supply device and an electric vehicle power supply device.
Here, for convenience of explanation, a power supply device for a low altitude satellite will be described.
[0002]
FIG. 6 is a configuration diagram of a low-altitude satellite power supply device using a storage battery such as a conventional NiCd (nickel cadmium) battery. In FIG. 6, 1 is a solar cell, 2 is a surplus power generated by the solar cell 1. The shunt device 3 to be consumed inputs the current of the solar cell 1 through the shunt device 2, supplies the current to the charging controller 4a and the load 6, and when the generated power of the solar cell 1 decreases, the storage battery 5 This is a power controller that controls the charging controller 4a so as to supply a current to the load 6 by discharging. The charge controller 4a receives the output of the power controller 3, supplies current to the storage battery 5 to charge, and charge control for discharging the storage battery 5 with a signal when the generated power of the solar battery 1 decreases. It is a vessel. Reference numeral 7 denotes a backflow prevention diode.
[0003]
The operation of the conventional low-altitude satellite power supply device will be described below.
The current from the solar cell 1 is input to the power controller 3 via the backflow prevention diode 7 and the shunt device 2. The power controller 3 supplies the current from the solar cell 1 obtained during sunshine to the load 6 and the charge controller 4a. The charge controller 4a generates a constant current I0 shown in FIG. 7C by the electric power from the power controller 3, supplies the current I0 to the storage battery 5, and charges the storage battery 5. The voltage of the storage battery 5 rises as shown in FIG. As shown in FIG. 7A, the voltage of the storage battery 5 has reached a preset temperature compensated voltage value (this is called a VT curve and is set from one to n as required). When detected by the charge controller 4a, the charge controller 4 shifts from the constant current charge so far to the constant voltage charge. As a result, the charging current decreases in a tapered manner as shown in FIG. 7C, and overcharge to the storage battery 5 is prevented.
On the other hand, when the generated power of the solar cell 1 decreases in the shade, the charge controller 4 a discharges the storage battery 5 by the output of the power controller 3 and supplies power to the load 6.
[0004]
[Problems to be solved by the invention]
The charging of the storage battery in the conventional low-altitude satellite power supply device is performed as described above. However, the constant voltage / constant current charging as described above is performed for the entire storage battery in which n storage battery cells are connected in series. Therefore, there has been a problem that a specific cell in the storage battery is overcharged due to an imbalance of charging characteristics of each cell constituting the storage battery. In particular, Li-Ion (lithium ion) cells composed of Li (lithium) electrodes have higher energy density, charging voltage, discharge voltage, etc. than NiCd cells and are expected to be used for storage batteries. In the case of a Li-Ion cell, there is a problem that when the battery is overcharged beyond the specified voltage, the electrode deterioration is promoted and the life is shortened. For example, the constant voltage operating voltage on the VT curve at the temperature To ° C is detected by adding the n cell voltages as the storage battery voltage and comparing with the set voltage. If the cell voltage is higher than the cell voltage due to the internal resistance of the cell, the upper limit voltage of the cell may be exceeded, resulting in deterioration of the cell.
[0005]
This invention is made in order to solve this subject, and it aims at obtaining the battery electrical storage apparatus which can ensure appropriate charge amount without the individual cell which comprises a storage battery being overcharged. .
[0006]
[Means for Solving the Problems]
The battery power storage device according to the first aspect of the invention is different from the storage battery in which the storage battery cells are cascade-connected to the storage battery until a plurality of different charging currents for charging the storage battery are generated from a power supply output, and different specified voltage values are obtained. Charging current generating means having means for supplying a plurality of charging currents.
[0007]
A battery power storage device according to a second invention generates a plurality of different charging currents in the charging current generating means in the first invention, and supplies the charging current at a low level after first supplying the charging current at a high level. Is provided with means for changing the charging current.
[0008]
According to a third aspect of the present invention, in the first and second aspects, the charging current generating means changes the charging current from a high level to a low level when one of the voltages of each storage battery cell reaches a specified voltage. Means are provided.
[0009]
A battery power storage device according to a fourth aspect of the present invention is the first to third aspects of the invention, wherein a shunt circuit is connected to each storage battery cell, and the voltage of any storage battery cell is defined in a state where a minimum charge current is supplied to the storage battery When the voltage is reached, the charging current flowing through the storage battery cell is bypassed to the shunt circuit connected to the storage battery cell.
[0010]
A battery power storage device according to a fifth invention is provided between the power source and the storage battery in the first to fourth inventions, and is normally turned on, and when any of the voltages of the storage battery cells reaches a specified voltage, A switch that is turned off by the charging current generating means and is turned on by discharging is provided.
[0011]
A battery power storage device according to a sixth aspect of the present invention is the first to fifth aspects of the invention, wherein the charging current generating means detects the voltage of the entire storage battery cell, and is charged at a constant voltage when the detected voltage reaches a specified voltage. Means for shifting to control is provided.
[0012]
A battery power storage device according to a seventh aspect of the present invention is the first to sixth aspects of the present invention, wherein the charging current generating means cancels the constant voltage charging control when the plurality of storage battery cell voltages are unbalanced, and the low level charging is performed. Means for charging until a specified voltage is reached with a current is provided.
[0013]
A battery power storage device according to an eighth invention uses a Li-Ion storage battery cell composed of a Li (lithium) electrode as the storage battery cell in the first to seventh inventions.
[0014]
DETAILED DESCRIPTION OF THE INVENTION
Embodiment 1 FIG.
FIG. 1 is a configuration diagram of a low-altitude satellite power supply apparatus according to Embodiment 1 of the present invention. In FIG. 1, 1, 2, 3, 5, 6, and 7 are the same as those in FIG. 4b is a charge controller that generates a plurality of charging currents based on the output of the charging solar cell 9 and supplies different charging currents to the storage battery 5 in which the storage battery cells are connected in cascade, and 8 is the charging solar cell 9 and the storage battery. 5 is a switch connected between the storage battery 5 and the backflow prevention diode 8, and is in an ON state at the start of charging. From the charging solar battery 9 to the direct storage battery 5 Charging is performed. Reference numeral 11 denotes a control diode.
The charge controller 4b includes a current control unit that generates charging currents I2 and I3 (I2> I3) that are lower in level than the charging current I1 based on the output of the charging solar cell 9.
A plurality of cell voltage detectors 12 are provided corresponding to the respective storage battery cells, detect the voltage of each storage battery cell, and output a predetermined signal when the detected voltage of the storage battery cell reaches a specified voltage , 13 is an OR circuit that is connected to the output terminals of the plurality of cell voltage detectors 12 and outputs a predetermined signal from the cell voltage detector 12 to the charge controller 4b.
[0015]
Next, the operation of the present invention will be described below.
When a charging current I1 (for example, 30 A) from the charging solar battery 9 is supplied to the storage battery 5 via the switch 10 as indicated by I1 in FIG. 2A, each storage battery cell of the storage battery 5 is charged and each The voltage of the storage battery cell rises as shown in FIG. The cell voltage detector 12 detects the voltage of each storage battery cell, but detects the cell voltage when any one of the plurality of storage battery cells reaches a specified voltage (eg, 3.98 V). For example, a high level signal is output from the device 12 to the OR circuit 13. When the charge controller 4b receives a high level signal output from the cell voltage detector 12 via the OR circuit 13, the charge controller 4b sends a signal for switching the switch 10 in the ON state to OFF via the control diode 11 to the switch 10. Output, and switch 10 is turned OFF. Further, the charging controller 4b is configured to turn off the switch 10 and shift to constant voltage charging when the entire storage battery cell voltage reaches a specified voltage (for example, 3.95V × the number of storage battery cells).
Further, the charging controller 4b generates a charging current I2, I3 (I2> I3) at a level lower than the charging current I1 based on the output from the charging solar cell 9 (the charging current I1 is changed to the charging currents I2, I3). For example, 5 A of charging current I2 (see I2 in FIG. 2A) is supplied to the storage battery 5 to charge each storage battery cell. At this time, the charging voltage of each storage battery cell initially decreases as shown in FIG. 2B, but then increases. When each storage battery cell is charged by the charging current of I2 and any one of the plurality of storage battery cells reaches a specified voltage (eg, 3.98 V), this is detected by the cell voltage detector 12, and the signal Is input to the charging controller 4b through the OR circuit 13. The charge controller 4b receives the signal from the cell voltage detector 12, switches the I2 to the charge current I3, and supplies the storage battery 5 with the charge current I3 (for example, 1A) shown in FIG. The cell is charged (see c in FIG. 2B).
The charging controller 4 b outputs a signal for returning the switch 10 to ON when the storage battery 5 is discharged to the switch 10 via the control diode 11.
[0016]
As described above, the present invention provides a multi-stage charging function in which a plurality of different charging currents are supplied to a storage battery, and the charging current is supplied at the first high level and then at the next lower level. The charging controller only needs to control a charging current at a level lower than the power of the charging solar cell, and the charging efficiency is improved, and there is an effect that it can be reduced in size and weight.
In addition, finer charge control can be performed by setting a lower level charge current.
[0017]
Embodiment 2. FIG.
FIG. 3 is a configuration diagram of a low-altitude satellite power supply device showing Embodiment 2 of the present invention. In the second embodiment, the shunt circuit 14 is connected in parallel to each storage battery cell in the configuration of the second embodiment, and when the voltage of the storage battery cell reaches the specified voltage, the charging current reaches the specified voltage. It is characterized in that the shunt circuit 14 connected in parallel to the storage battery cell is bypassed to suppress the voltage increase of the storage battery cell.
In the case where the battery is charged with the charging current I3, the cell voltage detector 12 outputs a low level signal when the voltage of the storage battery cell does not reach the specified voltage. The shunt circuit 14 is in an OFF state when the low level signal is output, and the charging current I3 flows through the storage battery cell. On the other hand, the cell voltage detector 12 outputs a high level signal when the voltage of the storage battery cell reaches a specified voltage. The shunt circuit 14 is turned on by this high level signal. As a result, the charging current is bypassed and consumed by the shunt circuit 14 connected in parallel to the storage battery cell that has reached the specified voltage, so that the charging current I3 does not flow through the storage battery cell, and the voltage rise can be suppressed.
[0018]
As described above, according to the present invention, the upper limit voltage can be controlled for each storage battery cell, so that the cycle life deterioration of the storage battery cell can be minimized.
[0019]
Embodiment 3 FIG.
FIG. 4 is a configuration diagram of a low-altitude satellite power supply device showing Embodiment 3 of the present invention. The third embodiment is basically the same as the second embodiment, but differs from the second embodiment in that a signal diode 19 that outputs a signal for turning off the switch 10 based on the output of the OR circuit 19; When the battery is charged with the charging current I3, the voltage of the entire storage battery is monitored, and when the voltage reaches a specified voltage (set lower than the specified voltage for switching the charging current), the constant voltage charging is performed from the constant current charging. The charging controller 4c having a function of shifting (switching) to is provided.
The constant voltage charging occurs when the storage battery cell voltages are balanced, and is an ideal state for battery operation.
[0020]
As described above, the present invention monitors the voltage of the entire storage battery when it is charged with the charging current I1, and from the constant current charging when the voltage reaches a specified voltage (eg, 3.95V × the number of storage batteries). Since the charge controller has a function to switch to constant voltage charging, and this function is used in combination with multistage charging, charging control is performed without operating the shunt circuit as much as possible when the voltage characteristics of the storage battery cells are balanced. The specified voltage can be kept low, and the cycle life deterioration of the storage battery cell can be kept low. .
[0021]
Embodiment 4 FIG.
FIG. 5 is a configuration diagram of a low-altitude satellite power supply apparatus showing Embodiment 4 of the present invention. The fourth embodiment is basically the same as the third embodiment, but is different from the third embodiment in that an imbalance occurs in each storage battery cell voltage after shifting from constant current charging to constant voltage charging. In such a case, the constant voltage charging control is canceled, and each storage battery cell voltage is forcibly charged with the charging current I3 until the shunt circuit 12 operates (until the shunt voltage), and the charging has a function of balancing each storage battery cell voltage. A controller 4d is provided.
The voltage of each storage battery cell is detected by the cell voltage detector 12 and input to the charge controller 4d via the OR circuit 13, and the charge controller 4d unbalances each storage battery cell voltage (each storage battery cell with respect to the specified voltage). The voltage of each storage battery cell is monitored on the ground station side, and when the imbalance occurs, the charging controller 4d is charged at a constant voltage. The control may be canceled to generate a command for charging each storage battery cell voltage with the charging current I3 until the shunt circuit 12 is forcibly operated.
[0022]
As described above, the present invention cancels the constant voltage charging control when each storage battery cell voltage is unbalanced after shifting from constant current charging to constant voltage charging, and shunts each storage battery cell with the charging current I3. By charging up to the operating voltage, it is possible to correct the imbalance of each battery cell voltage that occurs as the charging cycle progresses.
[0023]
Each of the above embodiments has been described by taking the power supply device for a low altitude satellite as an example, but the present invention can also be applied to other satellites, electric vehicles, terrestrial solar power generation, and the like.
[0024]
【The invention's effect】
According to this invention, the overcharge of a storage battery cell can be suppressed by charging the several storage battery cell cascade-connected by different charging current (multistage charging).
[0025]
Further, according to the present invention, when the voltage of any of the storage battery cells reaches a specified voltage in a state where the charging current is supplied to the storage battery at the lowest level, the charging current flowing through the storage battery cell is transferred to the shunt circuit connected to the storage battery cell. Since it bypasses, the overcharge of a storage battery cell can be suppressed.
[0026]
The present invention monitors the voltage of the entire storage battery in a state where the voltages of the storage battery cells are balanced, and when the voltage reaches a specified voltage, the constant current charging is switched to the constant voltage charging. The battery operation can be brought into an ideal state in order to suppress the life deterioration.
[0027]
Moreover, this invention, after shifting from constant current charging to constant voltage charging, when an imbalance occurs in each storage battery cell voltage, by releasing the constant voltage charging control and charging each storage battery cell to the shunt operating voltage, Unbalance of each battery cell voltage can be corrected.
[Brief description of the drawings]
FIG. 1 is a configuration diagram of a low-altitude satellite power supply apparatus according to Embodiment 1 of the present invention.
FIG. 2 is a diagram for explaining current and voltage characteristics of a low-altitude satellite power supply device according to Embodiment 1 of the present invention;
FIG. 3 is a configuration diagram of a low-altitude satellite power supply apparatus according to Embodiment 2 of the present invention.
FIG. 4 is a configuration diagram of a low-altitude satellite power supply apparatus according to Embodiment 3 of the present invention.
FIG. 5 is a configuration diagram of a low-altitude satellite power supply apparatus according to Embodiment 4 of the present invention.
FIG. 6 is a configuration diagram of a conventional low-altitude satellite power supply device.
FIG. 7 is a diagram for explaining current and voltage characteristics of a conventional low-altitude satellite power supply device.
[Explanation of symbols]
4 Charge Controller 5 Storage Battery 9 Charging Solar Battery 10 Switch 11 Control Diode 12 Cell Voltage Detector 13 OR Circuit 14 Shunt Circuit 16 Signal Diode.

Claims (6)

複数の蓄電池セルが縦続接続された蓄電池と、
電源の出力電流に基づいて上記蓄電池を充電するための充電電流を生成する充電制御手段と、
上記電源と蓄電池の間に接続されたスイッチと、を備え、
上記充電制御手段は、
上記スイッチの接続がＯＮ状態にて、上記各蓄電池セルの電圧のいずれかが規定電圧に達したときに上記スイッチの接続をＯＦＦ状態とした後、
上記いずれかの蓄電池セルの電圧が規定電圧に達した場合、生成する充電電流を高いレベルから低いレベルに変化させて上記蓄電池に供給し、
上記蓄電池全体の電圧が規定電圧に達したときに上記蓄電池を定電圧充電制御する、
ことを特徴とするバッテリ蓄電装置。A storage battery in which a plurality of storage battery cells are connected in cascade;
Charging control means for generating a charging current for charging the storage battery based on an output current of a power source;
A switch connected between the power source and the storage battery,
The charge control means includes
After the switch connection is turned on, when any of the voltages of the storage battery cells reaches a specified voltage, the switch connection is turned off .
When the voltage of any one of the storage battery cells reaches a specified voltage, the charging current to be generated is changed from a high level to a low level and supplied to the storage battery ,
When the voltage of the entire storage battery reaches a specified voltage, the storage battery is controlled at a constant voltage,
A battery power storage device. 各電池セルにそれぞれ接続され、上記蓄電池への充電電流供給状態でいずれかの蓄電池セルの電圧がシャント電圧に達した場合、当該蓄電池セルに流れる充電電流をそれぞれバイパスするシャント回路を備えたことを特徴とする請求項１記載のバッテリ蓄電装置。  Each battery cell is provided with a shunt circuit that bypasses the charging current flowing through the storage battery cell when the voltage of any storage battery cell reaches the shunt voltage in the state of charging current supply to the storage battery. The battery power storage device according to claim 1. 上記充電制御手段は、上記各蓄電池セルの電圧のモニタ結果に基づいて当該各蓄電池セルのセル電圧がアンバランスになったときに上記定電圧充電制御を解除し、上記低いレベルの充電電流で全ての蓄電池セルがシャント電圧に達するまで充電電流を供給することを特徴とする請求項２に記載のバッテリ蓄電装置。  The charging control means cancels the constant voltage charging control when the cell voltage of each storage battery cell becomes unbalanced based on the monitoring result of the voltage of each storage battery cell, The battery power storage device according to claim 2, wherein a charging current is supplied until the storage battery cell reaches a shunt voltage. 上記電源を構成する主電源で発生した電力を上記蓄電池に供給するとともに、当該主電源の発生電力が低下した場合には上記蓄電池を放電させるように上記充電制御手段を制御する電力制御手段を更に備え、
上記充電制御手段は、上記電源を構成する充電用電源の出力に基づいて当該充電用電源の電力より低いレベルの充電電流を生成することを特徴とする請求項１から請求項３のいずれかに記載のバッテリ蓄電装置。Power control means for supplying power generated by a main power source constituting the power source to the storage battery, and for controlling the charge control means to discharge the storage battery when the generated power of the main power source decreases. Prepared,
The charging control means generates a charging current at a level lower than the power of the charging power source based on the output of the charging power source constituting the power source. The battery power storage device described. 複数の蓄電池セルが縦続接続された蓄電池と、
電源出力から上記蓄電池を充電するための充電電流を生成する充電制御手段と、
上記各蓄電池セルにそれぞれ接続され、いずれかの蓄電池セルの電圧がシャント電圧に達した場合、当該蓄電池セルに流れる充電電流をそれぞれバイパスするシャント回路と、を備え、
上記充電制御手段は、
上記いずれかの蓄電池セルの電圧が規定電圧に達した場合、充電電流を高いレベルから低いレベルに変化させるとともに、
当該低いレベルの充電電流にて充電されている場合に、上記蓄電池全体の電圧が規定電圧に達したときに上記蓄電池を定電圧充電制御し、
上記各蓄電池セルの電圧のモニタ結果に基づいて当該各蓄電池セルのセル電圧がアンバランスになったときに上記定電圧充電制御を解除し、上記低いレベルの充電電流で全ての蓄電池セル電圧がシャント電圧に達するまで充電電流を供給する、
ことを特徴とするバッテリ蓄電装置。A storage battery in which a plurality of storage battery cells are connected in cascade;
Charging control means for generating a charging current for charging the storage battery from a power output;
A shunt circuit that is connected to each of the storage battery cells and bypasses a charging current flowing through the storage battery cell when the voltage of any of the storage battery cells reaches a shunt voltage;
The charge control means includes
When the voltage of any of the above storage battery cells reaches a specified voltage, the charging current is changed from a high level to a low level,
When charging with the low level charging current, when the voltage of the entire storage battery reaches a specified voltage, the storage battery is controlled at a constant voltage,
The constant voltage charging control is canceled when the cell voltage of each storage battery cell becomes unbalanced based on the monitoring result of the voltage of each storage battery cell, and all storage battery cell voltages are shunted at the low level charging current. Supply charging current until the voltage is reached,
A battery power storage device. 上記蓄電池セルはLi（リチウム）系電極で構成されるLi-Ion
（リチウムイオン）蓄電池セルを用いたことを特徴とする請求項１〜５のいずれか記載のバッテリ蓄電装置。The above storage battery cell is composed of Li-Ion electrodes
The battery power storage device according to claim 1, wherein a (lithium ion) storage battery cell is used.
JP15779799A 1999-06-04 1999-06-04 Battery power storage device Expired - Fee Related JP3736205B2 (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
JP15779799A JP3736205B2 (en) 1999-06-04 1999-06-04 Battery power storage device
US09/443,286 US6373224B1 (en) 1999-06-04 1999-11-19 Battery accumulating apparatus
FR9915100A FR2794578B1 (en) 1999-06-04 1999-11-30 BATTERY ACCUMULATION DEVICE
EP00108803A EP1058367B1 (en) 1999-06-04 2000-04-26 Battery accumulating apparatus
CA002310357A CA2310357C (en) 1999-06-04 2000-05-31 Battery accumulating apparatus

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP15779799A JP3736205B2 (en) 1999-06-04 1999-06-04 Battery power storage device

Publications (3)

Publication Number Publication Date
JP2000350378A JP2000350378A (en) 2000-12-15
JP2000350378A5 JP2000350378A5 (en) 2004-12-24
JP3736205B2 true JP3736205B2 (en) 2006-01-18

Family

ID=15657506

Family Applications (1)

Application Number Title Priority Date Filing Date
JP15779799A Expired - Fee Related JP3736205B2 (en) 1999-06-04 1999-06-04 Battery power storage device

Country Status (5)

Country Link
US (1) US6373224B1 (en)
EP (1) EP1058367B1 (en)
JP (1) JP3736205B2 (en)
CA (1) CA2310357C (en)
FR (1) FR2794578B1 (en)

Families Citing this family (50)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2002186192A (en) 2000-12-18 2002-06-28 Mitsubishi Electric Corp Battery charger
US8431264B2 (en) 2002-08-09 2013-04-30 Infinite Power Solutions, Inc. Hybrid thin-film battery
US8404376B2 (en) 2002-08-09 2013-03-26 Infinite Power Solutions, Inc. Metal film encapsulation
US8394522B2 (en) 2002-08-09 2013-03-12 Infinite Power Solutions, Inc. Robust metal film encapsulation
US9793523B2 (en) 2002-08-09 2017-10-17 Sapurast Research Llc Electrochemical apparatus with barrier layer protected substrate
US8021778B2 (en) 2002-08-09 2011-09-20 Infinite Power Solutions, Inc. Electrochemical apparatus with barrier layer protected substrate
US8445130B2 (en) 2002-08-09 2013-05-21 Infinite Power Solutions, Inc. Hybrid thin-film battery
US20070264564A1 (en) 2006-03-16 2007-11-15 Infinite Power Solutions, Inc. Thin film battery on an integrated circuit or circuit board and method thereof
US8236443B2 (en) 2002-08-09 2012-08-07 Infinite Power Solutions, Inc. Metal film encapsulation
US8728285B2 (en) 2003-05-23 2014-05-20 Demaray, Llc Transparent conductive oxides
TWI253195B (en) * 2003-12-26 2006-04-11 Ind Tech Res Inst Charging method and system for serially connected batteries
DE602005017512D1 (en) 2004-12-08 2009-12-17 Symmorphix Inc DEPOSIT OF LICOO2
US7959769B2 (en) 2004-12-08 2011-06-14 Infinite Power Solutions, Inc. Deposition of LiCoO2
JP2007014163A (en) * 2005-07-01 2007-01-18 Fujitsu Ltd Charging ic, charger and electronic apparatus
JP2007097330A (en) * 2005-09-29 2007-04-12 Kyocera Corp Charger and terminal apparatus
US7509688B2 (en) * 2005-10-20 2009-03-31 Steven Ross Gregg Facial hair trimmings catcher
WO2008039471A2 (en) 2006-09-29 2008-04-03 Infinite Power Solutions, Inc. Masking of and material constraint for depositing battery layers on flexible substrates
US8197781B2 (en) 2006-11-07 2012-06-12 Infinite Power Solutions, Inc. Sputtering target of Li3PO4 and method for producing same
US20080218127A1 (en) * 2007-03-07 2008-09-11 O2Micro Inc. Battery management systems with controllable adapter output
KR101407941B1 (en) 2007-04-16 2014-06-18 한라비스테온공조 주식회사 Solar cell system for Vehicles and its control method
WO2009001502A1 (en) * 2007-06-22 2008-12-31 Panasonic Corporation Nonaqueous secondary battery, battery pack, power supply system, and electrical device
JP2009032668A (en) * 2007-06-22 2009-02-12 Panasonic Corp Nonaqueous secondary battery, battery pack, power source system, and electrically powered equipment
KR100998302B1 (en) 2007-12-07 2010-12-06 삼성에스디아이 주식회사 Method for charging of secondary battery and charging device
US8268488B2 (en) * 2007-12-21 2012-09-18 Infinite Power Solutions, Inc. Thin film electrolyte for thin film batteries
TWI441937B (en) 2007-12-21 2014-06-21 Infinite Power Solutions Inc Method for sputter targets for electrolyte films
KR101606183B1 (en) 2008-01-11 2016-03-25 사푸라스트 리써치 엘엘씨 Thin film encapsulation for thin film batteries and other devices
KR101672254B1 (en) * 2008-04-02 2016-11-08 사푸라스트 리써치 엘엘씨 Passive over/under voltage control and protection for energy storage devices associated with energy harvesting
US20100026240A1 (en) * 2008-07-30 2010-02-04 3M Innovative Properties Company Lithium ion battery pack charging system and device including the same
CN102119454B (en) 2008-08-11 2014-07-30 无穷动力解决方案股份有限公司 Energy device with integral collector surface for electromagnetic energy harvesting and method thereof
JP2010068571A (en) * 2008-09-09 2010-03-25 Hitachi Koki Co Ltd Charging apparatus
KR101613671B1 (en) 2008-09-12 2016-04-19 사푸라스트 리써치 엘엘씨 Energy device with integral conductive surface for data communication via electromagnetic energy and method thereof
US8508193B2 (en) 2008-10-08 2013-08-13 Infinite Power Solutions, Inc. Environmentally-powered wireless sensor module
CN101953015A (en) * 2009-01-07 2011-01-19 松下电器产业株式会社 Battery set charging method and battery charging system
US20100231162A1 (en) * 2009-03-16 2010-09-16 Gm Global Technology Operations, Inc. Solar powered battery charging methods and devices for lithium-ion battery systems
US8599572B2 (en) 2009-09-01 2013-12-03 Infinite Power Solutions, Inc. Printed circuit board with integrated thin film battery
JP5525862B2 (en) * 2010-02-26 2014-06-18 三洋電機株式会社 Charger, program
JP5489779B2 (en) * 2010-02-26 2014-05-14 株式会社Ｎｔｔファシリティーズ Lithium-ion battery charging system and charging method
US9722334B2 (en) * 2010-04-07 2017-08-01 Black & Decker Inc. Power tool with light unit
US20110300432A1 (en) 2010-06-07 2011-12-08 Snyder Shawn W Rechargeable, High-Density Electrochemical Device
JP5541982B2 (en) * 2010-06-28 2014-07-09 シャープ株式会社 DC power distribution system
TWM402554U (en) * 2010-11-10 2011-04-21 Richtek Technology Corp Charger circuit
JP2012222837A (en) * 2011-04-04 2012-11-12 Toshiba Mitsubishi-Electric Industrial System Corp Secondary battery charge control system
DE102011017599A1 (en) * 2011-04-27 2012-10-31 Robert Bosch Gmbh Method for operating a storage device for storing electrical energy and storage device for storing electrical energy
EP2724445A4 (en) * 2011-06-21 2015-09-30 Husqvarna Ab System and method for charging of a rechargeable battery
DE102011121940A1 (en) * 2011-12-22 2013-06-27 Andreas Stihl Ag & Co. Kg Debalancing protection circuit for a battery pack
US8981709B1 (en) * 2012-08-22 2015-03-17 Edee, LLC Supplemental electrical generation apparatus and method
US9156359B2 (en) 2012-09-28 2015-10-13 GM Global Technology Operations LLC Methods and vehicle systems for selectively using energy obtained from a solar subsystem
CN103023112B (en) * 2012-12-18 2015-09-09 北车风电有限公司 The back-up source charging device of wind generating set pitch control system and charging method
FR3033674B1 (en) 2015-03-10 2018-04-06 Sunna Design ELECTRONIC CONTROL BOARD OF ENERGY CONTROL OF AUTONOMOUS AND COMMUNICABLE ELECTRICAL EQUIPMENT
JP7200512B2 (en) * 2018-06-21 2023-01-10 カシオ計算機株式会社 ELECTRONIC DEVICE, ELECTRONIC WATCH AND BATTERY CHARGING METHOD

Family Cites Families (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4079303A (en) 1976-07-28 1978-03-14 The United States Of America As Represented By The United States Department Of Energy Charging system and method for multicell storage batteries
US4270080A (en) 1978-12-14 1981-05-26 Sun Electric Corporation Automatic battery charge apparatus and method
JPS5972941A (en) 1982-10-20 1984-04-25 日本電気株式会社 Storage battery charging controller
JP3231801B2 (en) * 1991-02-08 2001-11-26 本田技研工業株式会社 Battery charger
JPH06133465A (en) 1992-08-27 1994-05-13 Sanyo Electric Co Ltd Method and apparatus for charging secondary battery
JPH06165399A (en) 1992-11-24 1994-06-10 Nippon Moriseru Kk Charger for lithium ion secondary cell
US5367244A (en) * 1993-01-19 1994-11-22 Premier Engineered Products, Inc. Battery charging method with stepped current profile and associated charger
US5530335A (en) * 1993-05-11 1996-06-25 Trw Inc. Battery regulated bus spacecraft power control system
JP3577751B2 (en) 1993-12-24 2004-10-13 ソニー株式会社 Battery charging device, battery pack, and battery charging method
US5550453A (en) 1994-01-24 1996-08-27 Motorola, Inc. Battery charging method and apparatus
FR2725849B1 (en) * 1994-10-18 1996-12-20 Accumulateurs Fixes METHOD FOR REGULATING THE CHARGE OF AN ELECTRIC BATTERY ASSEMBLY AND ARRANGEMENT USING THE SAME
CA2169706A1 (en) * 1995-03-03 1996-09-04 Troy Lynn Stockstad Circuit and method for battery charge control
JPH0997629A (en) 1995-09-29 1997-04-08 Sanyo Electric Co Ltd Plural lithium ion secondary battery charging method
JP3620118B2 (en) 1995-10-24 2005-02-16 松下電器産業株式会社 Constant current / constant voltage charger
JP3629791B2 (en) * 1996-01-17 2005-03-16 日産自動車株式会社 Charge control device for battery pack
GB9605830D0 (en) 1996-03-20 1996-05-22 Atomic Energy Authority Uk Cell overcharge prevention
JPH09308126A (en) 1996-05-17 1997-11-28 Nissan Motor Co Ltd Charger
US5729116A (en) * 1996-12-20 1998-03-17 Total Battery Management, Inc. Shunt recognition in lithium batteries
JP3884802B2 (en) 1996-11-07 2007-02-21 日産自動車株式会社 Lithium-ion battery charging method
JPH10191574A (en) * 1996-12-26 1998-07-21 Japan Tobacco Inc Charging equipment
JPH10248177A (en) 1997-03-03 1998-09-14 Sanyo Electric Co Ltd Charging circuit
US5804944A (en) 1997-04-07 1998-09-08 Motorola, Inc. Battery protection system and process for charging a battery
US5952815A (en) * 1997-07-25 1999-09-14 Minnesota Mining & Manufacturing Co. Equalizer system and method for series connected energy storing devices
JPH1189106A (en) 1997-09-08 1999-03-30 Central Res Inst Of Electric Power Ind Multi-stage charging method/device for secondary battery
US6034506A (en) * 1998-01-16 2000-03-07 Space Systems/Loral, Inc. Lithium ion satellite battery charge control circuit
JP2000236631A (en) 1999-02-17 2000-08-29 Nec Corp Battery charge control circuit

Also Published As

Publication number Publication date
FR2794578A1 (en) 2000-12-08
EP1058367A2 (en) 2000-12-06
FR2794578B1 (en) 2003-10-17
US6373224B1 (en) 2002-04-16
CA2310357C (en) 2004-02-17
CA2310357A1 (en) 2000-12-04
JP2000350378A (en) 2000-12-15
EP1058367B1 (en) 2011-06-15
EP1058367A3 (en) 2002-11-20

Similar Documents

Publication Publication Date Title
JP3736205B2 (en) Battery power storage device
US6373226B1 (en) Method of controlling discharge of a plurality of rechargeable batteries, and battery assembly
US8054044B2 (en) Apparatus and method for balancing of battery cell'S charge capacity
KR101124803B1 (en) Charge Equalization Apparatus and Method
KR100885291B1 (en) Electric charger
US8531157B2 (en) Charging apparatus having overcharge protection and charging method for the same
JP5488877B2 (en) Electric tool
JP3931446B2 (en) Battery charge state adjustment device
US9413037B2 (en) Cell capacity adjusting device
US20210399558A1 (en) Battery control unit and battery system
US11843267B2 (en) Battery control unit and battery system
KR20060078967A (en) Balance charging control method of 2nd-series battery pack
JP2010110156A (en) Pack battery
JP3755043B2 (en) Chargeable / dischargeable power supply
JP3629791B2 (en) Charge control device for battery pack
JP2001008373A (en) Battery unit and charging method of battery
JPH08140278A (en) Charging/discharging protector for battery pack
JP2000166103A (en) Charging discharging control method
JP2003158827A (en) Charging method, charging device, and discharging controller for lithium ion battery
US11581747B2 (en) Power supply device
JPH10313544A (en) Overcharge preventing circuit, overdischarge preventing circuit and charge/discharge control circuit
WO2021241136A1 (en) Backup power supply device
KR20120015861A (en) Method for cell balancing using sub-cell
JP5775324B2 (en) Battery system
KR20160008106A (en) Active balancing apparatus for balancing battery cell voltage

Legal Events

Date Code Title Description
A521 Written amendment

Free format text: JAPANESE INTERMEDIATE CODE: A523

Effective date: 20040120

A621 Written request for application examination

Free format text: JAPANESE INTERMEDIATE CODE: A621

Effective date: 20040120

RD01 Notification of change of attorney

Free format text: JAPANESE INTERMEDIATE CODE: A7421

Effective date: 20040624

A977 Report on retrieval

Free format text: JAPANESE INTERMEDIATE CODE: A971007

Effective date: 20050413

A131 Notification of reasons for refusal

Free format text: JAPANESE INTERMEDIATE CODE: A131

Effective date: 20050419

A521 Written amendment

Free format text: JAPANESE INTERMEDIATE CODE: A523

Effective date: 20050613

A131 Notification of reasons for refusal

Free format text: JAPANESE INTERMEDIATE CODE: A131

Effective date: 20050712

A521 Written amendment

Free format text: JAPANESE INTERMEDIATE CODE: A523

Effective date: 20050909

TRDD Decision of grant or rejection written
A01 Written decision to grant a patent or to grant a registration (utility model)

Free format text: JAPANESE INTERMEDIATE CODE: A01

Effective date: 20051004

A61 First payment of annual fees (during grant procedure)

Free format text: JAPANESE INTERMEDIATE CODE: A61

Effective date: 20051017

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20081104

Year of fee payment: 3

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20091104

Year of fee payment: 4

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20091104

Year of fee payment: 4

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20101104

Year of fee payment: 5

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20111104

Year of fee payment: 6

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20121104

Year of fee payment: 7

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20121104

Year of fee payment: 7

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20131104

Year of fee payment: 8

LAPS Cancellation because of no payment of annual fees